Planets and Satellites: Kepler's Laws — Question 2

Section 13-6 · Physics pages 1994–1995

Question 2 Equal angular sweeps do not take equal times in an eccentric orbit For a Kepler orbit, areal velocity is constant: dA/dt = 1 2r2 ˙θ. Its apoapsis radius is three times its periapsis radius. M Orbital-plane schematic; the attracting source is at a focus, not the ellipse center. (a) Compare the instantaneous angular speeds at the two apsides. (b) Compare the times to sweep equal very small angles centered at those apsides.
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Question 2 - Solution Equal angular sweeps do not take equal times in an eccentric orbit M (a) Derivation and calculation Let h = r2 ˙θ = 2 ˙A, constant by the area law. At the apsides, r2 p ˙θp = r2 a ˙θa. Since ra = 3rp, ˙θp ˙θa = ( ra rp )2 = 9 . (b) Result and interpretation For equal small angular intervals δθ, δt = δA ˙A ≃r2δθ/2 h/2 = r2 h δθ. Thus lim δθ→0 δta δtp = r2 a r2p = 9 . For finite angular intervals, integrate r(θ)2/h instead of treating radius as constant. Physical check The satellite takes longer to sweep a given small angle near apoapsis, where its areal wedge is larger.

Question 2

Equal angular sweeps do not take equal times in an eccentric orbit

For a Kepler orbit, areal velocity is constant: dA/dt=12r2θ̇dA/dt=\tfrac12r^2\dot\theta. Its apoapsis radius is three times its periapsis radius.

Diagram shown in the original SVG worksheet.

  1. Compare the instantaneous angular speeds at the two apsides.

  2. Compare the times to sweep equal very small angles centered at those apsides.

Question 2 - Solution

Equal angular sweeps do not take equal times in an eccentric orbit

Diagram shown in the original SVG worksheet.

(a) Derivation and calculation

Let h=r2θ̇=2Ȧh=r^2\dot\theta=2\dot A, constant by the area law. At the apsides, rp2θ̇p=ra2θ̇a.r_p^2\dot\theta_p=r_a^2\dot\theta_a. Since ra=3rpr_a=3r_p, θ̇pθ̇a=(rarp)2=9.\boxed{\frac{\dot\theta_p}{\dot\theta_a}=\left(\frac{r_a}{r_p}\right)^2=9}.

(b) Result and interpretation

For equal small angular intervals δθ\delta\theta, δt=δAȦ≃r2δθ/2h/2=r2hδθ.\delta t=\frac{\delta A}{\dot A} \simeq\frac{r^2\delta\theta/2}{h/2}=\frac{r^2}{h}\delta\theta. Thus limδθ→0δtaδtp=ra2rp2=9.\boxed{\lim_{\delta\theta\to0}\frac{\delta t_a}{\delta t_p} =\frac{r_a^2}{r_p^2}=9}. For finite angular intervals, integrate r(θ)2/hr(\theta)^2/h instead of treating radius as constant.

Physical check

The satellite takes longer to sweep a given small angle near apoapsis, where its areal wedge is larger.